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Computational study of flow incidence effects on the aeroacoustics of low blade-tip Mach number propellers

  • Published:2022-01 Issue: Volume:120 Page:107275
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Romani GianlucaORCID,Grande Edoardo,Avallone FrancescoORCID,Ragni Daniele,Casalino Damiano

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference38 articles.

1. Fast-Forwarding to a Future of On-demand Urban Air Transportation;Holden,2016

2. Community noise of urban air transportation vehicles;Casalino,2019

3. Factors that Influence Community's Acceptance of Noise: An Introduction for Urban Air Mobility;Connors,2019

4. Aeroacoustics of Flight Vehicles: Theory and Practice. Volume 1: Noise Sources;Hubbard,1991

5. NASA Collaborative Research on the Ultra High Bypass Engine Cycle and Potential Benefits for Noise, Performance, and Emissions;Hughes,2013

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1. Computational aeroacoustic study of co-rotating rotors in hover;Aerospace Science and Technology;2024-10

2. Tandem-Rotor Noise in Low Advance Ratio Transitional Flight;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30

3. Efficient noise footprint computation for urban air mobility maneuvers in vertiport environments;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30

4. Numerical Investigation of Aerodynamics and Acoustics in Dual-Propeller Tip-to-Tip Gap Distances;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30

5. On the Use of Acoustic Analogy and Scale-Resolving Turbulent Flow Computations for Noise Sources Identification;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30
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